[IGSREPORT-24994] Wk 1928 IGLOS Final Orbits
acc at igs.org
acc at igs.org
Fri Jan 6 18:12:59 PST 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1928 (Dec 18, 2016 - Dec 24, 2016)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1928.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl1928[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1928 in the SP3 format.
igl19287.sum Combination Report for GPS Week 1928.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -13.9 ns
1 | -11.5 ns
2 | -13.3 ns
3 | -7.1 ns
4 | -6.5 ns
5 | -9.0 ns
6 | -4.0 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1928, 1a.1928).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.1928.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.1928.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 1928 summary. (Dec 18, 2016 - Dec 24, 2016)
Table 1.1928.a GPS week : 1928 MJD: 57740.0-57746.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -2 8 -29 12 .31 20 18 | --- --- --- ---
| 0 0 1 11 24 25 .03 | --- ---
cof n/a| 0 0 -2 0 -26 7 .28 22 20 | --- --- --- ---
| 1 0 1 16 30 29 .05 | --- ---
emx n/a| -1 0 4 -94 -44 -65 .10 22 21 | -17713 -1367 3049 10511
| 1 1 3 25 23 50 .06 | 12217 785
esx n/a| 0 -1 0 28 -16 15 -.16 22 19 | -16098 -1353 3153 13414
| 0 1 1 25 8 28 .06 | 3857 1200
gfz n/a| -1 0 -6 52 93 69 -.04 23 18 | 0 -1716 3056 10590
| 1 0 2 11 21 25 .09 | 0 1520
grg n/a| 1 1 2 -29 -2 46 -.31 27 24 | -8380 -1721 3074 10881
| 0 1 3 16 28 75 .06 | 3211 1206
iac n/a| 1 0 0 29 18 -43 -.11 20 20 | -10293 -649 3051 10535
| 1 1 2 28 75 97 .03 | 2624 782
mcc n/a| 3 0 33 109 10 419 -.54 205 205 | --- --- --- ---
| 13 8 13 122 177 721 .74 | --- ---
Table 1.1928.b GPS week : 1928 MJD: 57740.0-57746.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
'E' flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 7 10 9 11 12 11 15 |
R02 | 6 6 6 6 8 10 9 |
R03 | 6 7 6 8 8 8 6 |
R04 | 7 7 6 7 9 9 23 |
R05 | 11 16 16 15 11 15 14 |
R06 | 7 8 8 9 10 14 9 |
R07 | 7 6 6 9 8 7 8 |
R08 | 8 9 7 9 7 9 8 |
R09 | 9 10 10 11 11 14 12 |
R10 | 8 7 7 7 9 11 8 |
R11 | 8 7 7 9 10 10 10 |
R13 | 11 10 9 9 10 9 10 |
R14 | 16 14 18 16 19 20 15 |
R15 | 8 8 7 8 9 10 8 |
R16 | 11 13 10 13 15 15 18 |
R17 | 8 9 8 11 11 10 10 |
R18 | 8 11 8 9 8 9 8 |
R19 | 9 10 12 12 16 14 12 |
R20 | 12 12 12 13 16 13 15 |
R21 | 7 9 7 8 11 11 10 |
R22 | 7 8 8 7 8 10 10 |
R23 | 8 10 10 11 9 12 11 |
R24 | 12 14 13 18 19 16 16 |
R26 | 24 35 40 24 0 0 0 |
Table 1.1928.c GPS week : 1928 MJD: 57740.0-57746.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1928 0 | 62 47 -25 712 853 -2250 87.4 1310 1310 | -13859 0
brd 1928 1 | -9 15 -57 -164 339 989 86.7 1412 1412 | -11511 0
brd 1928 2 | 39 -18 -40 -310 2077 360 86.1 1278 1278 | -13319 0
brd 1928 3 | 4 -8 -60 334 3128 -822 85.3 1281 1281 | -7110 0
brd 1928 4 | -27 8 -72 34 958 -1335 85.6 1393 1393 | -6513 0
brd 1928 5 | -50 47 -23 48 356 -2534 86.5 1536 1536 | -8985 0
brd 1928 6 | 26 9 52 80 156 -1121 86.6 2603 2603 | -4000 0
-------------+------------------------------------------------------------+----------------
brd 1928 mean| 6 14 -32 105 1124 -958 86.3 1544 1544 | -9328 0
brd 1928 sdev| 39 25 41 335 1092 1282 .7 475 475 | 3709 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1928.0 GPS week: 1928 Day: 0 MJD: 57740
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -4 7 -19 30 .33 18 17 | --- --- --- ---
cof n/a| -2 1 -5 -16 4 43 .26 22 21 | --- --- --- ---
emx n/a| 0 0 4 -123 -59 -108 .04 18 18 | -20976 -2695 2791 10853
esx n/a| -1 0 1 5 -15 18 -.17 18 17 | -17491 -2829 2824 13356
gfz n/a| -3 1 -4 43 81 67 -.01 21 15 | 0 -3958 2790 10740
grg n/a| 2 0 1 -4 -62 158 -.31 26 23 | -12161 -3393 2814 11327
iac n/a| 2 1 1 60 55 -78 -.08 19 19 | -12288 -1489 2791 10615
mcc n/a| 18 -15 22 171 150 -393 -.23 200 200 | --- --- --- ---
Table 2.1928.1 GPS week: 1928 Day: 1 MJD: 57741
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 -1 3 -19 15 .30 19 17 | --- --- --- ---
cof n/a| 0 0 -2 -1 3 0 .30 20 18 | --- --- --- ---
emx n/a| 0 -2 -1 -115 -12 -127 .13 19 19 | -27525 -644 2833 10552
esx n/a| 0 -1 1 -8 -24 -13 -.10 22 18 | -17345 435 2866 13316
gfz n/a| -1 0 -5 63 101 66 .05 20 16 | 0 -20 2849 10519
grg n/a| 0 1 6 -26 8 30 -.35 29 24 | -10631 -1441 2856 10329
iac n/a| 1 0 2 35 -56 59 -.14 21 21 | -10858 -60 2825 10248
mcc n/a| 13 7 17 5 -177 55 -.60 174 174 | --- --- --- ---
Table 2.1928.2 GPS week: 1928 Day: 2 MJD: 57742
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -2 5 -2 -4 .28 21 18 | --- --- --- ---
cof n/a| -1 1 -3 13 -9 16 .31 24 23 | --- --- --- ---
emx n/a| -1 -1 2 -50 -31 -44 .08 24 24 | -20698 -2116 3100 10055
esx n/a| 0 1 1 36 -21 -21 -.09 17 15 | -8323 -2440 3136 12592
gfz n/a| -2 0 -4 48 105 53 .09 22 18 | 0 -3224 3097 9911
grg n/a| 1 -1 0 -22 -9 30 -.34 27 26 | -11828 -2884 3109 10134
iac n/a| 0 0 1 -7 -29 5 -.11 19 19 | -11571 -1138 3107 9735
mcc n/a| -1 2 41 -89 -183 748 .05 177 177 | --- --- --- ---
Table 2.1928.3 GPS week: 1928 Day: 3 MJD: 57743
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -3 -78 37 .31 21 20 | --- --- --- ---
cof n/a| 0 0 0 -14 -80 -2 .28 23 22 | --- --- --- ---
emx n/a| -4 0 7 -77 -80 12 .20 24 24 | -9807 -1421 3448 11498
esx n/a| 0 -1 0 21 -24 0 -.13 22 21 | -19655 -550 3517 14262
gfz n/a| 0 0 -4 58 61 119 -.08 22 19 | 0 -1644 3476 11638
grg n/a| 1 1 -3 -60 15 95 -.33 29 24 | -6333 -1353 3503 11936
iac n/a| 2 0 -2 27 106 -162 -.13 22 22 | -6455 89 3482 11544
mcc n/a| 3 6 59 114 -111 520 -.31 215 215 | --- --- --- ---
Table 2.1928.4 GPS week: 1928 Day: 4 MJD: 57744
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -4 -1 -36 -17 .30 22 17 | --- --- --- ---
cof n/a| 0 1 -1 18 -51 -28 .31 23 20 | --- --- --- ---
emx n/a| -1 -1 6 -98 -58 -107 .15 22 22 | 6488 -922 3087 11113
esx n/a| 0 0 1 67 -14 45 -.22 23 19 | -18627 -864 3132 14217
gfz n/a| -2 0 -6 64 111 34 -.03 25 19 | 0 -1580 3096 11383
grg n/a| 1 1 3 -27 8 91 -.21 23 20 | -5963 -979 3117 11756
mcc n/a| -10 7 35 232 73 -418 -1.99 163 163 | --- --- --- ---
Table 2.1928.5 GPS week: 1928 Day: 5 MJD: 57745
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 0 -4 28 -32 -17 .37 21 18 | --- --- --- ---
cof n/a| 0 0 -4 20 -23 -20 .18 22 20 | --- --- --- ---
emx n/a| 0 -1 9 -87 -50 -34 .02 22 22 | -24559 -1199 3106 9621
esx n/a| 0 0 0 27 0 53 -.17 23 19 | -17330 -2347 3115 12628
gfz n/a| -2 -1 -8 33 120 75 -.18 27 22 | 0 -1787 3093 9667
grg n/a| 3 4 2 -34 1 -68 -.25 27 24 | -7874 -2182 3104 10144
mcc n/a| -14 -8 25 249 30 857 -.89 208 208 | --- --- --- ---
Table 2.1928.6 GPS week: 1928 Day: 6 MJD: 57746
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -2 17 -20 42 .30 19 16 | --- --- --- ---
cof n/a| 0 0 -2 -15 -27 46 .35 22 19 | --- --- --- ---
emx n/a| 0 0 4 -111 -21 -47 .11 21 20 | -26918 -574 2983 9887
esx n/a| 0 -3 -3 50 -17 24 -.25 31 24 | -13917 -879 3483 13532
gfz n/a| -1 0 -9 56 74 69 -.09 23 17 | 0 200 2996 10273
grg n/a| 1 1 7 -32 22 -14 -.35 27 26 | -3871 179 3018 10542
mcc n/a| 18 -3 31 84 288 1568 .21 301 301 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
'E' stands for eclipsing satellites (earth).
'M' stands for eclipsing satellites (moon).
'X' stands for excluded from the statistics but included in IGL orbit.
'T' stands for Total long arc orbit RMS for all satellites.
'NE' stands for long arc orbit RMS for Non-Eclipsing satellites only.
'MEDI' stands for median of the centre's satellite RMS.
'MD'
Units: mm.
Table 3.1928.0 GPS week: 1928 Day: 0 MJD: 57740
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1375 12 15 13 11 13 25 13 --- 6 | 60 59 74 62 72 64 33 --- 65
R02 | 539 7 9 12 9 9 19 16 --- 5 | 66 61 71 60 62 68 20 --- 63
R03 | 814 8 11 14 8 13 23 18 157 6 | 77 74 78 72 75 66 24 48 71
R04 | 558 11 15 10 15 16 20 15 --- 6 | 71 72 65 62 69 59 27 --- 64
R05 | 598 14 24 17 20 18 50 19 --- 10 | 50 59 52 53 51 50 21 --- 48
R06 | 2313 16 23 13 11 12 22 13 --- 6 | 49 50 49 45 47 42 23 --- 46
R07 | 529 16 19 12 11 11 26 18 300 7 | 75 79 71 69 71 72 28 163 69
R08 | 1126 16 18 15 26 10 20 9 --- 7 | 67 70 73 93 85 70 30 --- 76
XR09 | 3811 17 16 12 --- 19 --- 13 --- 9 | 30 33 38 --- 36 --- 22 --- 30
R10 | 695 16 19 11 22 16 20 13 --- 7 | 34 35 35 52 39 36 28 --- 38
R11 | 1466 15 21 16 15 20 20 23 --- 8 | 61 65 61 56 50 53 53 --- 55
R13 | 823 35 37 25 17 29 22 12 --- 11 | 63 64 39 41 37 34 28 --- 39
R14 | 1907 32 31 30 18 47 33 43 --- 15 | 49 55 59 55 68 45 37 --- 49
R15 | 939 13 13 18 19 24 14 12 --- 7 | 50 52 42 56 35 46 31 --- 43
R16 | 994 13 29 22 27 25 34 26 --- 11 | 45 60 39 55 50 45 44 --- 44
R17E | 1091 18 11 15 22 17 24 9 --- 8 | 70 64 70 66 60 61 25 --- 64
R18E | 800 10 8 18 20 16 24 17 --- 8 | 69 65 70 66 62 77 30 --- 67
R19E | 877 20 33 15 14 24 24 20 --- 8 | 52 66 41 50 56 48 40 --- 46
R20E | 937 30 25 32 18 29 28 17 --- 11 | 49 45 41 35 36 35 22 --- 31
R21E | 2972 15 23 14 11 20 20 16 70 7 | 41 46 35 32 33 29 32 107 32
R22E | 1053 20 16 17 7 19 12 9 --- 6 | 46 45 39 38 38 44 33 --- 38
R23E | 1603 14 19 11 18 12 27 25 --- 8 | 41 38 46 45 34 39 35 --- 40
R24E | 1582 21 27 24 27 27 30 29 --- 11 | 84 88 96 109 86 96 66 --- 91
XR26E | ---- 23 189 --- --- --- --- 23 --- 23 | 30 152 --- --- --- --- 24 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1309 18 22 18 18 21 26 19 200 |T 55 62 55 57 54 53 31 106 51
WRMS | 1309 17 21 18 17 15 23 19 200 |NE 56 59 56 59 56 53 29 105 53
MEDI | 994 16 19 15 17 18 23 16 157 |MD 50 60 52 55 51 48 28 107 46
Table 3.1928.1 GPS week: 1928 Day: 1 MJD: 57741
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1153 22 24 15 14 21 32 24 --- 9 | 49 45 67 62 72 61 28 --- 58
R02 | 463 12 8 8 10 11 21 17 --- 6 | 40 49 50 46 52 34 22 --- 44
R03 | 1499 14 15 14 12 13 23 10 135 6 | 48 49 48 32 40 30 24 36 39
R04 | 502 12 17 12 11 10 24 17 --- 6 | 37 45 43 41 39 30 17 --- 35
R05 | 532 21 24 29 23 18 77 31 --- 15 | 35 45 45 35 40 43 17 --- 33
R06 | 2728 14 16 16 11 24 24 14 --- 7 | 32 37 35 28 37 21 19 --- 29
R07 | 835 10 8 12 15 13 14 12 261 5 | 48 45 51 39 45 58 26 59 46
R08 | 1320 11 9 12 33 13 31 17 --- 9 | 45 48 50 71 58 33 22 --- 48
XR09 | 3208 18 21 12 --- 21 --- 13 --- 9 | 31 29 36 --- 41 --- 19 --- 30
R10 | 798 9 12 11 22 18 17 13 --- 6 | 36 38 40 42 36 45 21 --- 38
R11 | 1882 13 14 13 18 17 19 12 --- 7 | 77 80 77 72 70 78 29 --- 74
R13 | 2315 32 34 12 18 27 17 14 --- 9 | 52 53 34 46 34 31 21 --- 35
R14 | 1643 33 32 29 40 29 25 22 --- 13 | 33 52 41 46 55 36 32 --- 36
R15 | 880 16 19 17 21 18 18 12 --- 7 | 52 49 42 52 46 44 26 --- 44
R16 | 500 19 15 30 28 26 46 25 --- 13 | 40 39 29 42 52 39 38 --- 32
R17E | 1344 19 19 18 10 24 24 15 --- 8 | 77 80 71 68 76 58 29 --- 68
R18E | 1042 14 8 23 42 18 25 15 --- 10 | 54 56 46 83 61 47 29 --- 55
R19E | 857 25 23 20 13 26 28 18 --- 10 | 63 60 49 49 50 56 46 --- 49
R20E | 1047 26 25 22 24 22 33 27 --- 11 | 50 47 34 46 45 43 28 --- 36
R21E | 994 16 17 16 23 20 16 23 71 8 | 43 44 35 51 46 40 35 68 39
R22E | 2241 15 20 22 11 18 17 14 --- 7 | 50 54 52 48 42 51 22 --- 45
R23E | 1564 28 32 20 20 15 18 25 --- 10 | 31 30 39 41 37 36 31 --- 34
R24E | 1783 16 24 30 21 30 30 47 --- 13 | 71 71 71 74 78 76 43 --- 64
XR26E | ---- 34 69 --- --- --- --- 35 --- 35 | 46 69 --- --- --- --- 21 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1411 19 20 19 22 20 29 21 174 |T 47 50 47 50 50 45 26 54 43
WRMS | 1411 17 18 19 18 16 24 21 174 |NE 43 46 45 46 47 41 24 47 41
MEDI | 1153 16 19 16 18 18 24 17 135 |MD 46 48 45 46 46 43 26 59 39
Table 3.1928.2 GPS week: 1928 Day: 2 MJD: 57742
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 867 27 16 17 16 20 23 19 --- 9 | 50 63 66 78 76 67 41 --- 68
R02 | 470 11 14 19 13 11 10 12 --- 5 | 45 46 61 50 46 51 20 --- 48
R03 | 1376 10 11 15 7 10 22 16 133 6 | 61 64 66 59 62 75 25 48 60
R04 | 513 9 13 10 12 14 22 12 --- 6 | 50 50 48 38 41 62 16 --- 44
R05 | 1005 24 31 58 13 19 65 23 --- 16 | 41 55 59 41 44 28 17 --- 36
R06 | 2678 15 19 19 16 22 14 15 --- 7 | 39 42 34 27 33 32 14 --- 27
R07 | 857 7 10 11 14 16 18 11 243 5 | 52 52 56 52 56 48 29 113 52
R08 | 1131 13 22 11 10 8 20 21 --- 6 | 51 50 48 56 57 42 33 --- 53
XR09 | 2828 17 21 17 --- 20 --- 15 --- 10 | 39 41 36 --- 35 --- 19 --- 32
R10 | 884 10 21 13 15 17 23 12 --- 6 | 37 43 41 40 33 28 19 --- 34
R11 | 1093 19 21 12 10 22 17 8 --- 6 | 85 85 83 88 80 95 24 --- 85
R13 | 1596 32 40 19 10 23 24 11 --- 9 | 55 62 38 42 39 30 22 --- 36
R14 | 1867 46 41 38 42 30 46 38 --- 18 | 62 70 71 81 86 63 35 --- 63
R15 | 747 15 22 16 12 18 22 12 --- 7 | 52 55 42 48 37 37 20 --- 41
R16 | 640 19 34 27 22 28 18 21 --- 10 | 38 45 45 55 58 38 35 --- 45
R17E | 1821 19 18 17 16 21 26 9 --- 8 | 63 61 53 50 47 59 24 --- 51
R18E | 1518 15 14 16 15 22 17 21 --- 8 | 66 68 66 66 64 67 33 --- 63
R19E | 1361 25 33 33 14 31 31 20 --- 11 | 55 65 36 50 67 50 41 --- 45
R20E | 1039 23 24 30 19 29 36 28 --- 12 | 48 52 39 48 53 43 32 --- 40
R21E | 847 14 23 15 13 19 20 17 133 7 | 41 46 26 37 42 33 28 79 33
R22E | 1082 12 13 23 14 21 18 15 --- 7 | 46 50 47 43 45 45 20 --- 40
R23E | 1154 21 31 19 19 23 25 26 --- 10 | 32 31 43 48 41 44 30 --- 38
R24E | 1361 26 22 35 20 33 32 23 --- 12 | 40 42 47 49 61 56 37 --- 42
XR26E | ---- 40 65 --- --- --- --- 38 --- 39 | 39 67 --- --- --- --- 26 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1278 21 24 24 17 22 27 19 177 |T 49 54 50 52 52 49 26 80 45
WRMS | 1278 18 23 24 15 18 26 19 177 |NE 50 54 52 53 52 49 24 80 48
MEDI | 1093 17 21 17 14 21 22 16 133 |MD 48 52 47 49 47 45 25 79 42
Table 3.1928.3 GPS week: 1928 Day: 3 MJD: 57743
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 844 23 19 18 20 26 32 21 --- 10 | 61 65 74 81 82 61 41 --- 72
R02 | 520 13 20 9 16 10 20 10 --- 6 | 53 56 55 64 53 48 22 --- 53
R03 | 1261 11 16 22 11 20 31 12 133 8 | 59 58 64 56 55 47 22 52 54
R04 | 549 9 11 11 18 16 25 16 --- 7 | 59 62 54 68 69 49 19 --- 58
R05 | 800 31 31 34 41 23 49 18 --- 14 | 57 54 78 47 47 38 28 --- 48
R06 | 1622 24 25 15 22 19 18 15 --- 8 | 52 53 52 36 31 56 15 --- 41
R07 | 602 16 14 14 29 12 29 16 298 9 | 69 65 71 49 63 85 29 221 62
R08 | 749 23 20 19 20 14 24 14 --- 8 | 62 71 70 78 74 91 34 --- 72
XR09 | 2646 17 16 20 --- 19 --- 17 --- 10 | 42 42 46 --- 39 --- 20 --- 35
R10 | 707 8 10 19 20 14 19 16 --- 7 | 63 65 73 68 55 68 21 --- 60
R11 | 788 19 19 21 16 25 17 21 --- 9 | 138 139 146 133 128 139 41 --- 132
R13 | 1105 30 36 20 16 25 12 10 --- 9 | 62 58 37 44 35 40 20 --- 38
R14 | 3054 36 46 37 41 27 48 28 --- 16 | 47 57 53 64 54 64 38 --- 48
R15 | 826 15 12 14 18 16 26 19 --- 8 | 83 77 68 76 66 70 24 --- 69
R16 | 685 17 23 45 24 18 41 18 --- 12 | 70 70 84 83 74 55 33 --- 70
R17E | 1239 24 21 24 20 29 32 11 --- 10 | 99 96 88 68 82 100 27 --- 82
R18E | 2392 19 17 18 13 17 21 25 --- 8 | 70 71 61 65 58 70 58 --- 61
R19E | 848 29 22 22 17 35 19 24 --- 11 | 52 54 48 45 57 39 41 --- 41
R20E | 799 24 34 32 19 32 34 25 --- 12 | 49 53 45 51 51 42 31 --- 40
R21E | 819 14 9 20 14 18 22 16 181 7 | 49 48 42 43 39 52 39 158 43
R22E | 812 13 25 13 13 18 14 18 --- 6 | 71 76 63 63 67 67 19 --- 62
R23E | 1205 22 18 27 19 17 16 30 --- 10 | 37 49 51 50 46 37 41 --- 40
R24E | 2186 25 29 36 30 36 49 53 --- 17 | 74 82 86 99 94 71 47 --- 76
XR26E | ---- 24 126 --- --- --- --- 22 --- 23 | 60 152 --- --- --- --- 29 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1280 21 23 24 22 22 29 22 215 |T 64 69 65 65 61 63 30 143 58
WRMS | 1280 20 22 24 21 19 24 22 215 |NE 65 66 68 67 61 65 27 136 60
MEDI | 826 19 20 20 19 19 24 18 181 |MD 60 62 63 64 57 56 29 158 54
Table 3.1928.4 GPS week: 1928 Day: 4 MJD: 57744
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg mcc IGL | cod cof emx esx gfz grg mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1127 23 15 20 16 36 24 --- 12 | 43 51 64 57 64 56 --- 52
R02 | 555 13 14 21 13 11 15 --- 7 | 57 53 53 65 57 61 --- 57
R03 | 1399 16 27 18 13 21 14 146 8 | 62 70 64 64 47 55 68 57
R04 | 1119 13 12 12 16 10 27 --- 8 | 56 58 56 58 55 46 --- 53
R05 | 635 21 24 18 29 21 20 --- 11 | 53 62 55 50 51 50 --- 48
R06 | 1394 22 18 18 14 23 14 --- 9 | 49 48 40 44 47 40 --- 41
R07 | 525 12 21 11 19 10 21 118 7 | 60 64 52 52 57 63 96 56
R08 | 729 13 14 12 9 20 13 --- 6 | 52 49 52 53 63 53 --- 53
XR09 | 2655 13 21 12 --- 20 --- --- 11 | 40 47 37 --- 52 --- --- 42
R10 | 1011 7 22 12 25 14 21 --- 8 | 53 65 49 58 57 67 --- 55
R11 | 695 24 27 17 18 18 23 --- 10 | 151 155 148 146 155 155 --- 150
R13 | 796 21 27 12 19 25 17 --- 9 | 55 63 50 60 54 61 --- 53
R14 | 3402 37 44 25 51 33 36 --- 19 | 46 75 55 69 67 57 --- 50
R15 | 1014 14 24 19 12 15 23 --- 8 | 65 72 62 64 63 57 --- 60
R16 | 955 16 17 38 18 22 44 --- 15 | 57 55 53 62 60 53 --- 54
R17E | 972 22 22 22 21 23 16 --- 10 | 88 89 82 98 97 79 --- 87
R18E | 1366 12 14 21 11 17 18 --- 8 | 61 58 54 60 57 68 --- 57
R19E | 838 30 27 37 25 34 29 --- 15 | 58 56 49 52 57 47 --- 45
R20E | 2159 29 33 29 19 45 30 --- 15 | 57 54 47 55 66 53 --- 48
R21E | 705 21 17 19 23 26 17 210 10 | 52 48 42 46 45 43 100 42
R22E | 670 16 17 18 11 20 12 --- 8 | 49 47 51 45 41 41 --- 43
R23E | 814 18 19 19 21 17 14 --- 9 | 39 43 50 51 50 38 --- 42
R24E | 3047 39 32 39 42 46 21 --- 19 | 47 45 49 74 55 43 --- 45
XR26E | ---- 5 68 --- --- --- --- --- 0 | 40 117 --- --- --- --- --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1392 22 23 22 23 25 23 163 |T 57 64 57 62 61 58 88 55
WRMS | 1392 17 20 22 19 19 20 163 |NE 59 65 59 64 63 62 82 58
MEDI | 972 16 21 19 18 21 20 146 |MD 53 56 52 58 57 53 96 52
Table 3.1928.5 GPS week: 1928 Day: 5 MJD: 57745
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg mcc IGL | cod cof emx esx gfz grg mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 963 20 39 19 17 31 26 --- 11 | 37 41 19 27 47 45 --- 29
R02 | 658 17 16 19 13 19 27 --- 9 | 52 63 52 59 62 77 --- 57
R03 | 680 11 18 18 12 15 24 118 8 | 59 60 53 54 52 40 39 51
R04 | 1129 13 13 14 21 18 21 --- 8 | 55 50 46 52 48 57 --- 49
R05 | 652 21 24 26 39 14 41 --- 15 | 53 50 60 63 46 42 --- 48
R06 | 954 21 17 20 15 45 31 --- 13 | 54 55 54 54 57 48 --- 50
R07 | 866 14 17 14 11 10 19 96 7 | 61 59 55 49 50 60 75 53
R08 | 681 15 20 21 17 17 21 --- 9 | 50 51 47 31 56 46 --- 43
XR09 | 2351 17 11 12 --- 29 --- --- 14 | 37 37 38 --- 51 --- --- 38
R10 | 938 16 11 19 23 18 33 --- 11 | 61 64 61 60 58 83 --- 61
R11 | 998 20 25 17 16 22 21 --- 9 | 158 164 160 166 163 173 --- 162
R13 | 1709 20 15 12 9 27 16 --- 8 | 43 43 35 38 41 41 --- 37
R14 | 1930 33 33 43 47 43 27 --- 20 | 59 76 73 83 92 70 --- 70
R15 | 925 15 19 22 18 23 19 --- 9 | 66 69 58 64 58 60 --- 59
R16 | 1917 30 38 29 17 40 30 --- 14 | 63 62 51 59 62 47 --- 51
R17E | 1881 22 19 17 16 23 22 --- 10 | 103 103 87 86 91 94 --- 90
R18E | 755 16 18 18 19 20 18 --- 9 | 64 65 63 64 52 60 --- 59
R19E | 622 27 29 27 18 31 39 --- 14 | 56 57 45 44 49 60 --- 43
R20E | 1578 24 18 22 18 37 27 --- 13 | 49 46 37 44 48 51 --- 39
R21E | 1427 22 17 24 13 29 15 326 10 | 48 49 36 48 46 43 49 39
R22E | 1365 18 20 20 14 28 18 --- 10 | 72 77 63 65 64 69 --- 63
R23E | 844 15 20 18 32 16 33 --- 12 | 37 39 46 55 44 35 --- 39
R24E | 4644 24 23 20 44 31 37 --- 16 | 47 56 43 81 58 50 --- 51
XR26E | ---- 6 135 --- --- --- --- --- 0 | 22 160 --- --- --- --- --- 19
------+----------------------------------------------+------------------------------------------
RMS | 1535 21 22 22 23 27 27 207 |T 58 66 55 61 60 61 54 54
WRMS | 1535 18 20 22 19 22 24 207 |NE 60 62 57 61 62 63 57 57
MEDI | 963 18 19 19 17 23 24 118 |MD 54 57 52 55 52 51 49 50
Table 3.1928.6 GPS week: 1928 Day: 6 MJD: 57746
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg mcc IGL | cod cof emx esx gfz grg mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 807 17 30 23 30 35 41 --- 14 | 49 59 56 59 70 70 --- 57
R02 | 567 13 12 13 14 22 22 --- 8 | 67 71 67 64 72 70 --- 67
R03 | 1201 7 11 8 14 12 14 114 5 | 76 81 79 79 73 77 47 76
R04 | 9711 23 18 25 105 18 19 --- 23 | 72 74 65 91 75 71 --- 73
R05 | 663 16 16 21 36 30 35 --- 13 | 58 58 48 63 66 42 --- 50
R06 | 995 12 19 19 21 16 23 --- 9 | 64 66 65 60 59 47 --- 58
R07 | 738 14 17 12 8 12 28 200 8 | 82 83 79 71 75 74 100 75
R08 | 714 13 18 18 13 11 25 --- 8 | 72 74 73 69 72 66 --- 70
XR09 | 2642 16 16 10 --- 20 --- --- 11 | 34 41 39 --- 49 --- --- 38
R10 | 701 8 13 13 23 15 16 --- 7 | 54 54 65 66 56 55 --- 58
R11 | 955 18 12 12 21 19 25 --- 9 | 152 150 153 137 142 147 --- 146
R13 | 2959 24 29 14 17 24 20 --- 10 | 58 62 50 47 40 51 --- 46
R14 | 1788 24 40 22 34 34 31 --- 14 | 53 65 57 63 51 53 --- 52
R15 | 739 16 16 12 19 18 16 --- 8 | 65 67 58 53 50 52 --- 55
R16 | 1820 38 37 32 22 32 50 --- 18 | 80 66 64 70 65 85 --- 69
R17E | 2659 20 20 20 16 20 24 --- 10 | 107 105 104 94 103 88 --- 99
R18E | 601 12 11 14 17 12 20 --- 7 | 51 50 50 52 45 39 --- 46
R19E | 899 24 31 25 18 28 21 --- 12 | 55 62 48 36 40 44 --- 41
R20E | 1987 20 25 38 22 35 19 --- 14 | 52 56 43 50 66 47 --- 47
R21E | 1207 20 17 15 26 19 20 468 10 | 43 42 33 31 36 38 88 32
R22E | 1337 19 16 19 15 23 16 --- 9 | 60 60 59 54 46 52 --- 52
R23E | 916 21 24 23 27 19 24 --- 11 | 36 32 48 53 40 33 --- 39
R24E | 4038 13 19 36 36 32 44 --- 16 | 65 68 65 88 67 55 --- 63
XR26E | ---- 5 605 --- --- --- --- --- 0 | 31 494 --- --- --- --- --- 28
------+----------------------------------------------+------------------------------------------
RMS | 2602 19 22 21 31 23 27 301 |T 64 85 63 65 63 61 78 59
WRMS | 2602 16 19 20 24 17 26 301 |NE 69 71 67 70 67 68 73 66
MEDI | 995 16 18 19 21 20 22 200 |MD 58 65 59 63 65 53 88 55
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